View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36119U 09071A 24306.95333994 .24405297 24807-5 21681-3 0 9997
2 36119 97.1017 348.4694 0008698 256.9191 180.3364 16.51662681830030
| Epoch (UTC): | 01 November 2024 22:52:48 |
| Eccentricity: | 0.0008698 |
| inclination: | 97.1017° |
| perigee height: | 129 km |
| apogee height: | 140 km |
| right ascension of ascending node: | 348.4694° |
| argument of perigee: | 256.9191° |
| revolutions per day: | 16.51662681 |
| mean anomaly at epoch: | 180.3364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|